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  3. problem iii a small airplane has a total mass of...

Question: problem iii a small airplane has a total mass of...

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Problem III A small airplane has a total mass of 5000 kg and a wing area of 46m2, a lift coefficient of 0.5 at takeoff sittings. Determine a) the takeoff speed of the this aircraft. The air density at the sea level is p-1.18 kg/m b) the required power to maintain a constant cruising speed of 340 km/h for a cruising drag of 0.032 At this altitude the air density ρ-0.82 kg/m3

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